发明名称 |
Feather seal configuration for a gas turbine shroud |
摘要 |
<p>The assembly has multiple ring and spacer segments. Axial and radial sealing tongues (42, 44) are respectively housed in an axial slot (36) and a radial slot (38) placed oppositely in adjacent side faces of the segments. The axial slot of each segment has depth higher than depth of the radial slot. The axial tongue has width greater than the width of the radial tongue.</p> |
申请公布号 |
EP1593814(A1) |
申请公布日期 |
2005.11.09 |
申请号 |
EP20050290784 |
申请日期 |
2005.04.08 |
申请人 |
SNECMA |
发明人 |
GENDRAUD, ALAIN;ROUSSIN-MOYNIER, DELPHINE |
分类号 |
F01D9/04;F01D11/00;F01D25/00;F02C7/28;(IPC1-7):F01D11/00 |
主分类号 |
F01D9/04 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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